Add to ORKGWind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of sweepback were made at low speeds to evaluate the effects of the nacelle on the aerodynamic characteristics of the wing. Force, moment, and pressure-distribution measurements are presented for the nacelle underslung and centrally mounted on the wing and mounted on a strut below the wing
Tests were made in the NACA 19-foot pressure tunnel of a simplified twin-engine bomber model with an...
11 figs.Also published in J. Aircraft v. 20(7) p. 606-611 / FIZ - Fachinformationszzentrum Karlsruhe...
Tests were made i n the NASA-Ames 40- by 80-Foot Wind Tunnel of a wing semispan with a nacelle (no p...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Report presents the results of an experimental investigation made in the NACA full-scale wind tunnel...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
The present report, which deals with pressure-distribution measurements made on a sweptback wing wit...
Tests were made in the NACA 19-foot pressure tunnel of a simplified twin-engine bomber model with an...
11 figs.Also published in J. Aircraft v. 20(7) p. 606-611 / FIZ - Fachinformationszzentrum Karlsruhe...
Tests were made i n the NASA-Ames 40- by 80-Foot Wind Tunnel of a wing semispan with a nacelle (no p...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Report presents the results of an experimental investigation made in the NACA full-scale wind tunnel...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
The present report, which deals with pressure-distribution measurements made on a sweptback wing wit...
Tests were made in the NACA 19-foot pressure tunnel of a simplified twin-engine bomber model with an...
11 figs.Also published in J. Aircraft v. 20(7) p. 606-611 / FIZ - Fachinformationszzentrum Karlsruhe...
Tests were made i n the NASA-Ames 40- by 80-Foot Wind Tunnel of a wing semispan with a nacelle (no p...